N901AN

Part: HANDLE — UNSECURE (ZONE 800) · airframe 68,779 hrs · 28,789 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 17DEF OVERWING EMERGENCY EXIT DOOR HAS ESCAPE GRAB HANDLE IS FALLING DOWN. RESECURED GRAB HANDLE FOR OVERWING. PER AMM 52-20-01.

Part: CAP — UNSECURE (ZONE 200) · airframe 68,706 hrs · 28,753 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT END CAP AT SEAT 12C WILL NOT STAY ON. REINSTALLED SEAT EXIT LIGHT CAP AT ROW 12. PER AMM 33-51-03.

Part: BALLAST — BURNED OUT (ZONE 200) · airframe 68,354 hrs · 28,581 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANTS REPORT BURNT SMELL IN AFT GALLEY. PERFORMED JOB CARD 08L00021001. DURING TROUBLESHOOTING TRACED ODOR TO AFT GALLEY CEILING LIGHT ELECTRONIC BALLAST. ALSO, FOUND BALLAST OVERHEATING. REPLACED BALLAST, PER AMM 33-26-02. OPERATIONAL CHECK GOOD.

Part: LIGHT — DISCONNECTED (ZONE 200) · airframe 67,813 hrs · 28,319 cycles

AIRCRAFT WAS NOT GROUNDED: 31C EMERGENCY LIGHT PANEL DISCONNECTED FROM HOUSING. REINSTALLED EMERGENCY LIGHT ASSEMBLY ON SEAT 31C. PER MM 25-21-00.

Part: PANEL — CORRODED (ZONE 100) · airframe 67,783 hrs · 28,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT BULKHEAD PANEL 141TW AT BS 947, S10. REPAIRED PER SRM 51-10-02.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 67,783 hrs · 28,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER, RIGHT HAND WHEEL WELL, AT STA 663, FROM RBL 38 TO RBL 42. REPAIRED VAPOR BARRIER PER SRM 57-10-10-2R-2.

Part: SLIDE — WORN (ZONE 800) · airframe 67,783 hrs · 28,305 cycles

AIRCRAFT IN BASE MAINTENANCE: L2 PASSENGER DOOR EMERGENCY ESCAPE SLIDE PACK IS WORN AND FRAYED. REMOVED AND REPLACED L2 DOOR ESCAPE.

Part: BULKHEAD — DELAMINATED (MLG WW) · airframe 67,783 hrs · 28,305 cycles

AIRCRAFT IN BASE MAINTENANCE: AREA BELOW RIGHT HAND WHEEL WELL AFT BULKHEAD HAS DELAMINATED STRUCTURE PLIES. APPLIED PERMANENT REPAIR ON THE AREA BELOW THE RIGHT HAND WHEEL WELL AFT BULKHEAD. PER B737NG SRM 53-60-71-2R-1.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 67,783 hrs · 28,305 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK ENTRANCE AREA CENTER LEFT HAND FLOOR DENTED IN ON FRAME STRUCTURES. REMOVED AND REPLACED THE FLIGHT DECK.

Part: SILL DRAIN — CLOGGED (ZONE 200) · airframe 67,311 hrs · 28,103 cycles

AIRCRAFT WAS GROUNDED: AFTER ENGINES STARTED AS WE TAXIED CABIN CREW REPORTED STRONG ODOR IN AFT GALLEY. ACCOMPLISHED SMOKE ODOR FUMES INITIAL TROUBLE SHOOTING, PER J/C08L00021001. FOUND AFT DOOR SIL DRAIN CLOGGED REMOVED CLOGGED AND ACCOMPLISHED J/C 08L10038003 ACCOMPLISHED ENGINE RUN NO ODOR NOTED AT TIME.

Part: MODULE — INOPERATIVE (ZONE 800) · airframe 66,565 hrs · 27,750 cycles

AIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR WILL NOT UNLOCK WITH FLIGHT DECK DOOR CONTROL SWITCH ON CENTER CONSOLE. REMOVED AND REPLACED COCKPIT DOOR MODULE, OPERTIONAL CHECK GOOD. PER AMM 52-51-07.

Part: LIGHT — DETACHED (ZONE 200) · airframe 65,942 hrs · 27,433 cycles

AIRCRAFT WAS NOT GROUNDED: WHITE ESCAPE PATH LIGHT ON SEAT 18C IS DETACHED FROM THE SEAT BRACKET. REATTACHED BRACKET FOR EMERGENCY LIGHT MARKER LIGHT. OPERTIONAL CHECKS GOOD. PER AMM 25-42-02.

Part: HOUSING — DETACHED (ZONE 200) · airframe 65,726 hrs · 27,326 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT PANEL HANGING LOOSE AT SEAT 20C. INSTALLED NEW HOUSING AT SEAT 20C AND PREFORMED EMERGENCY LIGHT TEST GOPOD. PER AMM 33-51-00**(CLOSED).

Part: LIGHT — UNSECURE (SEAT 20C) · airframe 65,726 hrs · 27,326 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT PANEL HANGING LOOSE AT SEAT 20C. (OPEN).

Part: SENSOR — FAULTY (ZONE 700) · airframe 65,592 hrs · 27,258 cycles

AIRCRAFT WAS GROUNDED: NO EMERGENCY DECLARED DUE TO: WHEN GEAR WAS RETRACTED OUT OF LAS THE NOSE GEAR DID NOT RETRACT. GEAR EXTENDED DURING LANDING; AIRCRAFT LANDED SAFELY AT ORD. TROUBLESHOT, PER FIM 32-61-00-810-803. CONFIRMED SENSOR S853 FAULTY. REMOVED AND REPLACED S853 SENSOR, OPERTIONAL CHECK GOOD. PER AMM 32-61-51.

Part: GASKET — LEAKING (FUEL SYSTEM) · airframe 65,299 hrs · 27,123 cycles

AIRCRAFT WAS GROUNDED:RETURN TO GATE, ON TAXI-OUT ANOTHER AIRCRAFT REPORTED LIQUID STREAMING FROM RIGHT ENGINE. CABIN FILLED WITH ODOR OF FUEL AND WE SECURED THE RIGHT ENGINE AS A PRECAUTION. REMOVED AND REPALCED THE GASKET FUEL OUT TUBE FROM OIL COOLER RIGHT ENGINE. LEAK TESTED GOOD. PER AMM 73-11-06.

Part: FITTING — CRACKED (ZONE 100) · airframe 65,232 hrs · 27,089 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 54.60. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (BS 540 RBL41) · airframe 65,232 hrs · 27,089 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 40.87. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (BS 540) · airframe 65,232 hrs · 27,089 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (BS 540 LBL15) · airframe 65,232 hrs · 27,089 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 15.04. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (BS 540 LBL41) · airframe 65,232 hrs · 27,089 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 40.87. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (BS 540 LBL32.4) · airframe 65,232 hrs · 27,089 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (BS 540 LBL6) · airframe 65,232 hrs · 27,089 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 6.14. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (BS 540 RBL6) · airframe 65,232 hrs · 27,089 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 6.14. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (BS 540 LBL55) · airframe 65,232 hrs · 27,089 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 54.60. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (BS 540 RBL15) · airframe 65,232 hrs · 27,089 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 15.04. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: SIGN — LOOSE (CABIN) · airframe 65,231 hrs · 27,089 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR EXIT SIGN HAS A LOOSE BEZEL. REMOVED AND REPLACED R1 DOOR EXIT SIGN ASSEMBLY. PER B737-NG AMM 33-51-01-960-802 AND PERFORMED OPERATIONAL CHECK. PER B737-NG AMM 33-51-00-720-801 CHECKED GOOD.

Part: SIGN — BROKEN (CABIN) · airframe 65,231 hrs · 27,089 cycles

AIRCRAFT IN BASE MAINTENANCE: R1 DOOR EXIT SIGN HAS LOOSE BEZEL. REMOVED AND REPLACED R1 DOOR EXIT SIGN ASSEMBLY. OPERTIONAL CHECK GOOD. PER B737-NG AMM 33-51-01-00-720-801.

Part: FLASHLIGHT — NO TEST (FWD CABIN) · airframe 65,225 hrs · 27,085 cycles

AIRCRAFT WAS NOT GROUNDED: L1 JUMSEAT FLASHLIGHT INOPERATIVE. REPLACING FLASHLIGHT. OPERTIONAL CHECK GOOD. PER AMM 25-64-00.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 65,225 hrs · 27,085 cycles

AIRCRAFT WAS NOT GROUNDED: AFT JUMP SEAT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT AT AFT JUMP SEAT. OPERTIONAL CHECK GOOD. PER AMM 25-64-00.

Part: SIGN — OUT OF POSITION (ZONE 200 - FUSE) · airframe 64,330 hrs · 26,643 cycles

AIRCRAFT WAS NOT GROUNDED: AFT SIDE OF EMERGENCY EXIT SIGN IN CENTER AISLE CEILING NEAR EMERGENCY EXIT ROWS CAME OFF. RESECURED EXIT SIGN REAR COVER AS NEEDED. OPERATIONAL CHECK GOOD.

Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 63,855 hrs · 26,419 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT ON SEAT 12C BROKEN. REMOVED AND REPLACED THE SEAT LIGHT HOUSING. PER AMM 33-51-11. OPERATIONAL CHECK PASSED.

Part: SPRING — UNKNOWN (ZONE 800 - DOORS) · airframe 62,468 hrs · 25,703 cycles

AIRCRAFT WAS GROUNDED. L1 DOOR ARRIVED WITH EXTERIOR HANDLE NOT STOWED. REMOVED AND REPLACED BROKEN SPRING AT DOOR HANDLE MECHANISM.

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 62,375 hrs · 25,652 cycles

AIRCRAFT WAS NOT GROUNDED: PASSENGER AFT CABIN MEGAPHONE OVER SEAT 36 D.E.F DID NOT TEST PROPERLY. REPLACED BATTERIES OPERATION CHECKS NORMAL. OK FOR SERVICE.

Part: GIRT BAR — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 62,234 hrs · 25,583 cycles

AIRCRAFT WAS NOT GROUNDED: GIRT BAR ON R1 SERVICE DOOR VERY LOOSE. ADJUSTED GIRT BAR AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: NONE — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 61,974 hrs · 25,464 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR GIRT BAR CLIPS ARE TOO TIGHT. ADJUSTED GIRT BAR CLIPS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: RETAINER — OUT OF ADJUST (GIRT BAR) · airframe 61,514 hrs · 25,238 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS GIRT BAR ON SERVICE DOOR IS DIFFICULT TO STOW AND UNSTOW. ADJUSTED RETAINER CLIPS IAW AMM 25-61-01.

Part: SLIDING WINDOW — OUT OF ADJUST (COCKPIT RT) · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: HEAVY FORCE NEEDED TO CLOSE FIRST OFFICER`S WINDOW. ADJUSTED AND PERFORMED FUNCTIONAL CHECK OR R2 WINDOW IAW AMM 56-12-11, HANDLE FORCES ARE WITHIN LIMITS.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FIRST OFFICERS #1 WINDOW POST LOCATED AT BS 217 AND WL 258. REPAIRED WINDOW POST PER ECO 5616J009-008.

Part: VAPOR BARRIER — CRACKED (BS 663 BULKHEAD) · airframe 61,486 hrs · 25,226 cycles

CRACK IN LEFT WHEEL WELL, FORWARD VAPOR BARRIER. LOCATED AT BS 663.75 AND FROM LBL 45 TO LBL 54. REPAIRED VAPOR BARRIER IAW SRM 57-10-10-2R-2 PARAGRAPH 6 STEP D.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 61,518 hrs · 25,240 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WHEEL WELL SMALL CRACK IN FORWARD PART OF THE LEFT WHEEL WELL ACCOMPLISHED PERMANENT REPAIR ON LEFT WHEEL WELL VAPOR BARRIER AT LEFT BUTT LINE 54.21-45.64 STA. 663.75.

Part: BAFFLE — CRACKED (BS 500D-500E) · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT LEFT HAND FLOOR STRUCTURE BAFFLE ASSEMBLY LOCATED FROM BS 500E TO BS 500D AT LBL 16. REPLACED BAFFLE ASSEMBLY PER SRM 51-40-02.

Part: SKIN — DENTED (ZONE 300 - STABS) · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: DENT IN RIGHT HAND ELEVATOR UPPER SKIN LOCATED AT ELEVATOR STATION 216 AND STAB RBL 180. REPAIRED SKIN PER SRM 55-20-01-2R-1 AND SRM 51-70-04-2R-14.

Part: SKIN — DENTED (ZONE 300 - STABS) · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: DENT IN RIGHT HAND ELEVATOR UPPER SKIN LOCATED AT ELEVATOR STATION 186 AND STAB RBL 160. REPAIRED SKIN PER SRM 55-20-01-2R-1 AND SRM 51-70-04-2R-14.

Part: SKIN — DENTED (ZONE 300 - STABS) · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: DENT IN RIGHT HAND ELEVATOR UPPER SKIN LOCATED AT ELEVATOR STATION 140 AND STAB RBL 155. REPAIRED SKIN PER SRM 55-20-01-2R-1 AND SRM 51-70-04-2R-14.

Part: SKIN — PUNCTURED (RT ELEVATOR) · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: PUNCTURE IN RIGHT HAND ELEVATOR UPPER SKIN LOCATED AT ELEVATOR STA 70 AND RBL 140. REPAIRED SKIN PER SRM 55-20-01-2R-1 AND SRM 51-70-04-2R-1.

Part: SKIN — PUNCTURED (RT ELVATOR) · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: PUNCTURE IN RIGHT HAND ELEVATOR UPPER SKIN LOCATED AT ELEVATOR STA 93 AND RBL 150. REPAIRED SKIN PER SRM 55-20-01-2R-1 AND SRM 51-70-04-2R-1.

Part: SKIN — DELAMINATED (RT ELVATOR) · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED RIGHT HAND ELEVATOR UPPER SKIN LOCATED AT ELEVATOR STA 177 AND RBL 180. REPAIRED SKIN PER SRM 55-20-01-2R-1 AND SRM 51-70-04-2R-1.

Part: STRAP — CORRODED (R1 DOOR SILL) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R1 DOOR SILL INNER CHORD FORWARD STRAP LOCATED AT BS 322 AND RBL 62. REPLACED STRAP PER SRM 51-40-02-0G.

Part: STRINGER CLIP — CORRODED (BS 500E S6L) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER CLIP LOCATED AT BS 500E AND S6L. REPLACED STRINGER CLIP PER SRM 51-40-02-0G

Part: SPLICE PLATE — CORRODED (BS 500C RBL 16) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL SPLICE PLATE LOCATED AT BS 500C + 16 AND RBL 16.5. REPLACED TRANSITION PANEL SPLICE PLATE PER SRM 53-00-53-2R-5.

Part: SIDEWALL SUPPORT — CORRODED (BS 500D S26R) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SIDEWALL PANEL SUPPORT LOCATED AT BS 500D AND S26R. REPLACED PANEL SUPPORT PER SRM 51-40-02-0G.

Part: TRANSITION PANEL — CORRODED (BS 420-440) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL LOCATED FROM BS 420 TO BS 440 AT RBL 16. REPLACED TRANSITION PANEL PER SRM 51-40-02-0G.

Part: SEAT TRACK — DAMAGED (BS 727I RBL 45) · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: DAMAGE TO MAIN CABIN SEAT TRACK LOCATED AT BS 727I PLUS 16 INCHES AND AT RBL 45L. REPAIRED SEAT TRACK PER SRM 53-00-52-2R-5.

Part: CARGO TRACK — CORRODED (BS 500I) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT AFT RIGHT HAND LOWER CENTER RAIL LOCATED AT BS 500I FROM LBL 16.5 TO RBL 16.5. REPLACED RAIL PER SRM 51-40-02-0G.

Part: SUPPORT FITTING — DAMAGED (BS 492 RBL 20) · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE IN FORWARD CARGO COMPARTMENT FLOOR SUPPORT FITTING LOCATED AT BS 492 AND RBL 20. REPLACED SUPPORT FITTING PER SRM 51-40-02-0G.

Part: FLOOR SUPPORT — CRACKED (BS 500D) · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR INTERCOSTAL LOCATED AT BS 500D + 8 INCHES AND LBL 16.5. REPLACED INTERCOSTAL PER SRM 51-40-02-0G.

Part: FLOOR SUPPORT — CORRODED (BS 951 LBL 24) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR INTERCOSTAL LOCATED AT BS 951 AND LBL 24. REPLACED INTERCOSTAL PER SRM 51-40-02-0G.

Part: TRANSITION PANEL — CORRODED (BS 500A-500H) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL LOCATED FROM BS 500A TO BS 500H AT RBL 16.5. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R-5.

Part: SUPPORT — CORRODED (BS 500I S26L) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

FORWARD CARGO AFT LOWER LEFT SUPPORT CORRODED LOCATED AT STA 500I AND STR 26L. REMOVED AND REPLACED FORWARD CARGO AFT SUPPORT PER SRM 51-40-02-0G.

Part: TRANSITION PANEL — CORRODED (BS 492-500A) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL LOCATED FROM BS 492 TO BS 500A AT RBL 27. REPLACED TRANSITION PANEL PER SRM 51-40-02-0G.

Part: CREASE BEAM — CORRODED (BS 927-992 RBL54) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN CREASE BEAM INNER CHORD LOCATED FROM BS 927 TO BS 992.8 AT LBL 54. REPLACED CHORD PER SRM 51-40-02-0G.

Part: WEB — CORRODED (BS 1016 LBL 30) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR WEB LOCATED AT BS 1016 AND LBL 30. REPLACED WEB PER SRM 51-40-02-0G.

Part: WEB — CORRODED (BS 989 LBL 30) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR WEB LOCATED AT BS 989 AND LBL 30. REPLACED WEB PER SRM 51-40-02-0G.

Part: FLOORBEAM — CORRODED (BS 986 BL0-RBL46) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR BEAM LOCATED AT BS 986.5 AND FROM BL 0 TO RBL 46. REPAIRED FLOOR BEAM PER SRM 53-70-51-2R-4.

Part: CREASE BEAM — CORRODED (BS 951-992 RBL46) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN DECK CREASE BEAM CHORD LOCATED FROM BS 951 TO BS 992.8 AT RBL46. REPLACED CHORD PER SRM 51-40-02-0G.

Part: FLOOR SUPPORT — CORRODED (BS 992) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR PANEL SUPPORT Z ANGLE LOCATED AT BS 992.8 AND RBL 35. REPLACED FLOOR PANEL SUPPORT PER SRM 51-40-02-0G.

Part: FLOOR SUPPORT — CORRODED (BS 992-1060) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR PANEL SUPPORT LOCATED FROM BS 992.8 TO BS 1060 AT RBL 30. REPLACED SUPPORT PER SRM 53-70-51-1A AND SRM 51-40-02-0G.

Part: FLOORBEAM — CORRODED (BS 986 BL0-LBL46) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR BEAM T-CHORD LOCATED AT BS 986.5 AND FROM BL 0 TO LBL 46. REPLACED T-CHORD PER SRM 53-70-51-2R-4.

Part: FLOOR SUPPORT — CORRODED (BS 967-986) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: MAIN DECK AFT WET AREA BETWEEN STA 967 AND 986.5 AND LEFT BUTT LINE 17 APPROXIMATELY FLOOR SUPPORT UNDER SCREW HOLES CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02-0G.

Part: STRINGER CLIP — CRACKED (BS 500I S26R) · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO COMPARTMENT FLOOR STRUCTURE STRINGER CLIP HAS CRACKS LOCATED AT STA 500I AND STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02-0G.

Part: DOOR SILL — CORRODED (BS 320-345 LBL60) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: L1 DOOR LOWER SILL UPPER SURFACE CORRODED BETWEEN STA 320-345 AND LEFT BUTT LINE 60. REMOVED AND REPLACED L1 DOOR LOWER SILL PER SRM 51-40-02-0G.

Part: FLOORBEAM — CORRODED (BS 951 RBL 45-49) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR BEAM LOCATED AT BS 951 AND FROM RBL 45 TO RBL 49. REPAIRED FLOOR BEAM PER SRM 53-70-51-2R-5.

Part: FLOOR SUPPORT — CORRODED (BS 951 RBL25) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR INTERCOSTAL LOCATED AT BS 951 AND RBL 25. REPLACED INTERCOSTAL PER SRM 51-40-02-0G.

Part: PRESSURE BLKHD — NOT REPORTED (ZONE 100) · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: PREFORMED PERMANENT REPAIR TO RIGHT HAND VERTICAL PRESSURE DECK WEB LOCATED AT BS 663 FROM RBL 15 TO RBL 45. REPAIRED PER SRM 57-10-10-2R-3, AND EA 340218.

Part: FLOOR SUPPORT — CORRODED (BS 951 RBL 48) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR INTERCOSTAL LOCATED AT BS 951 AND RBL 48. REPLACED INTERCOSTAL PER SRM 51-40-02-0G.

Part: FLOORBEAM — CORRODED (BS 947 LBL 12-46) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR BEAM LOCATED AT BS 947.5 AND FROM LBL 12 TO LBL 46. REPAIRED FLOOR BEAM PER SRM 53-70-51-2R-5.

Part: STRINGER CLIP — CORRODED (BS 500E S6R) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER CLIP LOCATED AT BS 500E AND S6R. REPLACED STRINGER CLIP PER SRM 51-40-02-0G.

Part: SUPPORT BRACKET — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT BRACKET LOCATED AT BS 947.5 AND FROM RBL 12 TO RBL 22. REPLACED BRACKET PER SRM 51-40-02-0G.

Part: TRANSITION PANEL — CORRODED (BS 927-947) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL LOCATED FROM BS 927 TO BS 947.5 AND FROM RBL 19 TO RBL 22. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R.

Part: TRANSITION PANEL — CORRODED (BS 727I-767) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL LOCATED FROM BS 727I TO BS 767 AND FROM RBL 19 TO RBL 22. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R.

Part: TRANSITION PANEL — CORRODED (BS 760-787) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED FROM BS 760 TO BS 787 AND FROM LBL 19 TO LBL 22. REPAIRED TRANSITION PANEL PER SRM 53-00-53-2R-5.

Part: TRANSITION PANEL — CORRODED (BS 727G-727H) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED FROM BS 727G TO BS 727H AND FROM LBL 19 TO LBL 22. REPAIRED TRANSITION PANEL PER SRM 53-00-53-2R.

Part: TRANSITION PANEL — CRACKED (BS 727IR LBL22) · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED AT BS 727I AND LBL 22. REPAIRED TRANSITION PANEL PER SRM 53-00-53-2R.

Part: SUPPORT FRAME — CORRODED (WNG-BDY FAIRING) · corrosion level 2 · airframe 61,486 hrs · 25,226 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND WING TO BODY AFT FAIRING SUPPORT FRAME ASSEMBLY LOCATED AT BS 727 +2 AND RBL 9.5. REPAIRED FRAME ASSEMBLY PER EA 340107.

Part: CONTROL VALVE — FAILED (AC BAY) · airframe 59,827 hrs · 24,444 cycles

AIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO ORD ON ACCOUNT OF PRESSURIZATION PROBLEM. AN EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED FIM TASK 21-62-00-810-849, FOUND STANDBY TEMPERATURE CONTROL VALVE STAYS OPEN WHEN PACK IS RUNNING AND ALL SENSE LINES ARE DISCONNECTED. REMOVED AND REPLACED TEMP CONTROL VALVE IAW AMM 21-51-10. OPS CHECK GOOD NO LEAKS.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 59,436 hrs · 24,272 cycles

AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN FLOOR PANEL ATTACH ANGLE CRACKED AT BS 540 BETWEEN BL 0 AND LBL 4. REPLACED ATTACH ANGLE PER SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 59,436 hrs · 24,272 cycles

AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN FLOOR PANEL ATTACH ANGLE CRACKED AT BS 540 BETWEEN BL 0 AND RBL 4. REPLACED ATTACH ANGLE PER SRM 51-40-02.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 59,436 hrs · 24,272 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED VERTICAL PRESSURE WEB AT BS 663 BETWEEN RBL 25 AND RBL 45.64. REPAIRED VERTICAL PRESSURE WEB PER EA 295944 AND SRM 57-10-10-2R-4.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,436 hrs · 24,272 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL BETWEEN BS 328 AND BS 344 AT LBL 45. REPLACED INTERCOSTAL PER 51-00-05.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 59,436 hrs · 24,272 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED VERTICAL PRESSURE DECK WEB AT BS 663 BETWEEN RBL 31.83 AND RBL 40. REPAIRED VERTICAL PRESSURE DECK WEB PER EA 295944AND SRM 57-10-10-2R-4.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 59,435 hrs · 24,271 cycles

AIRCRAFT WAS GROUNDED: RIGHT HAND REAR SPAR VERTICAL PRESSURE DECK WEB CRACKED AT BS 663 AND RBL 29 AT WL 208. REPAIRED PRESSURE DECK WEB PER EA 295944.

Part: ENGINE — FIRE (NR 2) · airframe 58,974 hrs · 24,063 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS AFTER GATE ARRIVAL IN KIN, AND ENGINES AND APU SHUTDOWN. GROUND CREW REPORTED FIRE IN #'2 ENGINE. THERE WAS NO FIRE OR OVERHEAT INDICATION IN COCKPIT. FIRE WENT OUT, DURATION UNKNOWN, BUT LESS THAN 5 MINUTES CONTINUED. AIRPORT FIRE CREW INSPECTED ENGINE, NO FIRE NOTED. MAINTENANCE ACCOMPLISHED AMM 71-00-00-800-803-F00. NO FAULTS FOUND.

Part: FUEL SYS — MALFUNCTIONED · airframe 58,909 hrs · 24,028 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS DURING FLIGHT, PREMATURE FUEL BURN FROM BOTH WING TANKS WITH FUEL IN CENTER TANK. ALL PUMPS SHOW NORMAL. 1:40 HRS INTO FLIGHT, LOST 700 LBS IN RIGHT TANK AND 300 LBS FROM LEFT TANK. CENTER TANK IS FEEDING NORMAL. WHEN CENTER TANK WAS EMPTY, LEFT TANK HAD 8.0 AND RIGHT HAD 7.5. ACCOMPLISHED FQIS BITE TEST IAW, FIM 28-41-00, BITE TEST GOOD, NO FAULTS, MESSAGES NOTED. READY FOR NEXT STEP CHECK WHICH IS DRY CAP AND RESISTANCE CHECK IAW AMM 28-41-21. MAINTENANCE ACCOMPLISHED FIM TASK 28-41-00, SATISFACTORY RESULTS. REINSTATED CENTER RIGHT FUEL PUMP & OPS CHECKED NORMAL

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 58,324 hrs · 23,777 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN WAS FOUND CRACKED AT HSS 129.50. REPAIRED THE SKIN IAW RD 55-10-00-2

Part: SMOKE DETECTOR — FALSE INDICATION (AFT LAVATORY) · airframe 57,871 hrs · 23,575 cycles

RIGHT AFT LAVATORY SMOKE DETECTOR WAS FLASHING A RED LIGHT, NO SMOKE WAS SEEN. MAINTENANCE PERFORMED A SATISFACTORY OPERATIONAL CHECK IAW AMM 26-14-00.

Part: TRUNNION — CORRODED (LT MLG) · corrosion level 2 · airframe 57,069 hrs · 23,228 cycles

CORROSION ON THE LEFT MAIN LANDING GEAR FORWARD TRUNNION FITTING INBOARD LOWER HOLE. REPLACED THE TRUNNION FITTING IAW SRM 51-40-02, AND 51-00-05.

Part: TRUNNION — CORRODED (RT MLG) · corrosion level 2 · airframe 57,069 hrs · 23,228 cycles

CORROSION ON RIGHT MAIN LANDING GEAR FORWARD TRUNNION FITTING INBOARD LOWER HOLE. REPLACED THE TRUNNION FITTING IAW SRM 51-40-02, AND 51-00-05.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,905 hrs · 23,160 cycles

AIRCRAFT WAS GROUNDED. BATTERY M1695 FAILS CARD 2908. REPLACED BATTERY (M1695). OPERATIONS CHECK GOOD. REFERENCE AMM 33-51-06.

Part: PROXIMITY SENSOR — FAULTY (LE FLAP) · airframe 54,697 hrs · 22,162 cycles

THE AIRCRAFT WAS GROUNDED. AT OUTER MARKER OF LAX, RECEIVED NR 4 LE FLAP LEFT SIDE TRANSIT LIGHT AT FLAPS 10. THE FLIGHT LEVELED OFF AT 2000 FEET AND TRACKED THE LOCALIZER. AN EMERGENCY WAS DECLARED. RAN THE CHECKLIST FOR LEADING EDGE TRANSIT LIGHT. THE FLIGHT RETURNED TO LANDING ON 25L. WHEN THE GEAR CAME DOWN, THE TRANSIT LIGHT EXTINGUISHED. THE FLIGHT CONTINUED THE APPROACH USING QRH PROCEDURES. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. TROUBLE SHOT PER FIM 27-88-00. FOUND FAULT 27-81206. FOUND HIGH RESISTANCE ON SL4 PROX SENSOR OUTBOARD S1000. REMOVED AND REPLACED PROX SENSOR S1000 PER AMM 27-88-11. OPS TESTS GOOD.

Part: QUICK DISCONNECT — FAILED (HYDRAULIC SYS) · airframe 54,669 hrs · 22,150 cycles

THE AIRCRAFT WAS GROUNDED. AFTER GEAR RETRACTION LEFT ENGINE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. REMAINED ON.. FOLLOWED QRH PROCEDURES, DECLARED AN EMERGENCY, AND RETURNED TO DFW WITHOUT FURTHER INCIDENT. FOUND PYLON QUICK DISCONNECT FITTINGS FOR PRESSURE FOR ENG DRIVEN HYD PUMP FAILED. REMOVED AND REPLACED PRESSURE ,RETURN AND CASE DRAIN PYLON QUICK DISCONNECT FITTING PER MM 29-11-11,54-51-51 AND 20-50-11 OPS AND LK CKS GOOD.

Part: PUMP — FALSE INDICATION (FUEL BOOST) · airframe 53,686 hrs · 21,752 cycles

RIGHT CENTER TANK FUEL BOOST PUMP LOW PRESSURE LIGHT, DISAGREES WITH PUMP STATUS. PRIMED CENTER BOOST PUMPS IAW AMM 28-22-41-420-801. OPS CHECKED GOOD.

Part: BULKHEAD WEB — DAMAGED (BS 1016) · airframe 51,410 hrs · 20,826 cycles

LOOSE FASTENER FOUND TO HAVE CAUSED AN ELONGATED HOLE IN BS 1016 PRESSURE BULKHEAD AT APPROXIMATLEY S10L. OVERSIZED HOLE AND INSTALLED REPLACEMENT FASTENER IAW EA 262025.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 51,410 hrs · 20,826 cycles

INTERCOSTAL AT LBL 45 BETWEEN BS 312 - 328 IS CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW AARD 51-10-05-1.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 51,410 hrs · 20,826 cycles

VERTICAL PRESSURE WEB AT BS 663.75 IS CRACKED AT APPROXIMATELY LBL 45. REPAIRED WEB IAW SRM 57-10-10-2R-3 AND EA 262001.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 51,410 hrs · 20,826 cycles

FLOOR SUPPORT AT LBL 1 BETWEEN BS 344 - 360 IS CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW AARD 51-00-05-R1 AND DRAWING 141A5400.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 51,410 hrs · 20,826 cycles

FLOOR SUPPORT AT LBL 11 BETWEEN BS 344 - 360 IS CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW AARD 51-00-05-R1 AND DRAWING 141A5400.

Part: TRANSCEIVER — FAULTY (WEATHER RADAR) · airframe 51,390 hrs · 20,815 cycles

AIRCRAFT WAS GROUNDED. AIR INTERRUPT, EMERGENCY DECLARED, LANDING UNEVENTFUL, WEATHER RADAR TILT CONTROL INOPERATIVE. RADAR SHOWED SOLID GREEN OR YELLOW SCREEN. R & R WEATHER RADAR TRANSCEIVER IAW AMM 34-43-41. ACCOMPLISHED OPS TEST IAW AMM 34-43-00. SYSTEM CHECKS NORMAL.

Part: FSEU — FAULTY (TE FLAP) · airframe 50,316 hrs · 20,393 cycles

WHEN FLAPS 5 WERE SELECTED, THEY STOPPED AT 1.5 DEGREES. LOWERED TO 15 DEGREES WITH ALTERNATE FLAPS SWITCH. AN EMER WAS DECLARED & THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. REPLACED FSEU IAW AMM 27-51-01. ACCOMPLISHED ALL INSTALLATION TEST. NO SYS FAULTS. OK FOR SERVICE. THE ACFT WAS NOT GNDED.

Part: SLIDE — DETACHED (R1 DOOR) · airframe 50,005 hrs · 20,271 cycles

AIRCRAFT WAS GNDED. FOUND RI DOOR SLIDE DETACHED BUT NOT DEPLOYED. REINSTALLED DOOR SLIDE IAW AMM 25-66-01.

Part: SENSOR — FAULTED (TE FLAPS) · airframe 49,682 hrs · 20,142 cycles

FLAPS WOULD NOT DEPLOY PAST 2 DEGREE USING FLAP HANDLE. ALTERNATE FLAP PROCEDURE USED 15 DEGREE LANDING. EMERGENCY DECLARED, LANDING UNEVENTFUL, AND ACFT WAS GROUNDED. MAINTENANCE FOUND A PUSHED BACK PIN IN THE NR 8 FLAP SKEW SENSOR. REMOVED AND REPLACED FLAP SKEW SENSOR NR 8 IAW AMM 27-59-01.

Part: TRANSMITTER — OUT OF POSITION (TE FLAP) · airframe 49,660 hrs · 20,134 cycles

EMERGENCY LANDING DECLARED. INBD ACCOUNT FLAP ASYMMETRY MSGE. NON EVENTFUL LANDING. NO FURTHER INCIDENTS WERE REPORTED. ACFT WAS REMOVED FROM SERVICE. ACCOMPLISHED TE FLAP TRANSMISSION SERVICING ON FLAP TRANSMISSIONS 1, 3, 5 & 8 IAW AMM 12-22-51-610-803. REPOSITIONED LT FLAP POSITION TRANSMITTER IAW AMM 27-58-01-400-801.

Part: PROXIMITY SENSOR — FAULTY (LE FLAP) · airframe 49,431 hrs · 20,039 cycles

FLAPS REMAINED AT 5 WHEN HANDLE POSITIONED TO 10. THE FLIGHT ABORTED APPROACH. AN EMER WAS DECLARED & THE FLIGHT DIVERTED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. ACFT TAKEN OUT OF SERVICE. R & R NR 1 LE SLAT PROXIMITY OTBD SENSOR S994 IAW AMM 27-88-11. OPERATIONALLY CHECKED GOOD.

Part: SENSOR — FAILED (LE SLAT) · airframe 49,413 hrs · 20,032 cycles

ON APPROACH, EXTENDING FLAPS FROM 2 - 5 FLAPS STOPPED AT JUST BEYOND 2 DEGREES. SYMMETRICAL AT ALL TIMES. FLAPS EXTENDED TO 15 USING ALTERNATIVE FLAP SWITCH. FLIGHT DECLARED AN EMER & LANDED NORMAL. NO FLAP OVER SPEED THROUGHOUT. ACFT WAS REMOVED FROM SERVICE. FOUND LE4 SENSOR S175 OUT OF TOLERANCE. REPLACED S175 SENSOR. REQUIRED TESTS PASSED IAW MM 27-88-11.

Part: FLAP — MALFUNCTIONED (WING) · airframe 49,068 hrs · 19,890 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH, AFTER SELECTING FLAPS 5, FLAPS STOPPED AT 4. EMER CHECK LIST USED TO EXTEND MANUAL TO 15. ACCOMPLISHED OPERATIONAL CHECK OF FULL TRAVEL OF FLAPS & A BITE OF THE FSEU IAW 27-51-00-810-802, NO FAULTS NOTED.

Part: TRANSMITTER — DEFECTIVE (TE FLAP) · airframe 48,620 hrs · 19,719 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. FLAP LOCKOUT INDICATION ON APPROACH. REPLACED FLAP POSITION TRANSMITTER IAW AMM 27-58-01 & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,451 hrs · 19,651 cycles

FUSELAGE SKIN AT STATION 500 + 9 IS CORRODED BETWEEN STRINGER 28L & 28R. ACCOMPLISHED EXTERNAL DOUBLER REPAIR IAW SRM 53-00-01-2R-3.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 47,325 hrs · 19,179 cycles

EMERGENCY DECLARED AT DESTINATION LOCATION. LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. TE FLAPS DID NOT AGREE WITH FLAP HANDLE. LOWERED TO 15 WITH ALTERNATE FLAP SWITCH. ATTEMPTED TO LOWER FLAPS NORMALLY AT GEAR DOWN 170 KTS. FLAPS STAYED AT 5 DEGREES. COULD NOT FIND ANY FAULTS. FLAPS ARE OPERATING IAW AMM OPERATIONAL CHECKS. REPLACED THE HYD TE BYPASS VLV, PRECAUTIONARY, IAW AMM 27-51-02. SYS CHECKED NORMAL.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 45,191 hrs · 18,322 cycles

FASTENER HOLE CRACKED IN LOWER FLANGE OF LT HORIZONTAL STABILIZER RIB. INSTALLED REPAIR ANGLE IAW EA B737-55-035121.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,191 hrs · 18,322 cycles

STATION 727D HAS CRACK IN FRAME BETWEEN STRINGERS 20 & 21 RT. ACCOMPLISHED FRAME REPAIR.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 45,191 hrs · 18,322 cycles

TWO 1.5 INCH CRACKS IN LT HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STATION 129.5, 17 & 25 INCHES AFT OF THE FRONT SPAR. REPAIR DOUBLER INSTALLED IAW SRM 55-10-01.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 45,191 hrs · 18,322 cycles

CORROSION FOUND ON FUEL TANK SKIN. ACCOMPLISHED REPAIR IAW EA B737-57-034887.

Part: SUPPORT BEAM — WORN (FUSELAGE) · airframe 45,191 hrs · 18,322 cycles

CENTER WING SUPPORT BEAM WORN BEYOND LIMITS. ACCOMPLISHED REPAIR IAW EA B737-57-034997.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 45,191 hrs · 18,322 cycles

CORROSION FOUND ON RT CTR FUEL TANK SKIN AROUND DRAG BRACE. ACCOMPLISHED REPAIR IAW EA B737-57-034887.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,191 hrs · 18,322 cycles

SEVERAL EMER EXIT LIGHTS AT LT & RT OVERWING EXITS INOPERATIVE. REPLACED LT SIDEWALL BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 45,191 hrs · 18,322 cycles

LEFT NR 1 CREASE CHORD FROM STATIONS 945 TO 1005 & LBL 54 CORRODED. REPLACED CREASE ANGLE IAW AARD 51-10-05-1.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · airframe 45,191 hrs · 18,322 cycles

CORROSION ON TRANSITION PANEL. REPLACED PANEL IAW SRM 53-00-53-2R-6.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,191 hrs · 18,322 cycles

STATION 947 LAVATORY MOUNT CORRODED ON FLOORBEAM. ACCOMPLISHED T CAP REPAIR IAW SRM 53-70-51-2R-5.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 45,191 hrs · 18,322 cycles

CRACKS WERE DISCOVERED ON 727B LONGITUDINAL FLOORBEAM FLANGES AT LBL 54 OTBD FLANGES. ACCOMPLISHED NESTED ANGLE REPAIR IAW ECO J1698 & EA B737-53-034888.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 45,191 hrs · 18,322 cycles

CRACKS WERE DISCOVERED ON 727B LONGITUDINAL FLOORBEAM FLANGES AT RBL 54 OTBD FLANGES. ACCOMPLISHED NESTED ANGLE REPAIR IAW ECO J1698 & EA B737-53-034888.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 45,191 hrs · 18,322 cycles

CRACKS WERE DISCOVERED ON 727B LONGITUDINAL FLOORBEAM FLANGES AT LBL 24 INBD FLANGES. ACCOMPLISHED NESTED ANGLE REPAIR IAW ECO J1698 & EA B737-53-034888.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 45,191 hrs · 18,322 cycles

CRACKS WERE DISCOVERED ON 727B LONGITUDINAL FLOORBEAM FLANGES AT RBL 54 INBD FLANGES. ACCOMPLISHED NESTED ANGLE REPAIR IAW ECO J1698 & EA B737-53-034888.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 45,191 hrs · 18,322 cycles

CRACKS WERE DISCOVERED ON 727B LONGITUDINAL FLOORBEAM FLANGES AT RBL 24 OTBD FLANGES. ACCOMPLISHED NESTED ANGLE REPAIR IAW ECO J1698 & EA B737-53-034888.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 45,191 hrs · 18,322 cycles

CRACKS WERE DISCOVERED ON 727B LONGITUDINAL FLOORBEAM FLANGES AT LBL 24 OTBD FLANGES. ACCOMPLISHED NESTED ANGLE REPAIR IAW ECO J1698 & EA B737-53-034888.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 45,191 hrs · 18,322 cycles

CRACKS WERE DISCOVERED ON 727B LONGITUDINAL FLOORBEAM FLANGES AT LBL 54 INBD FLANGES. ACCOMPLISHED NESTED ANGLE REPAIR IAW ECO J1698 & EA B737-53-034888.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 45,191 hrs · 18,322 cycles

CRACKS WERE DISCOVERED ON 727B LONGITUDINAL FLOORBEAM FLANGES AT RBL 24 INBD FLANGES. ACCOMPLISHED NESTED ANGLE REPAIR IAW ECO J1698 & EA B737-53-034888.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 45,191 hrs · 18,322 cycles

LEFT NR 1 CREASE ANGLE CORRODED. REPLACED LT NR 1 CREASE ANGLE IAW AARD 51-00-005-01.

Part: ANGLE — CORRODED (R1 DOOR) · corrosion level 2 · airframe 45,191 hrs · 18,322 cycles

RIGHT NR 1 DOOR CREASE ANGLE CORRODED. R & R ANGLE IAW AARD 51-00-05-1.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 45,191 hrs · 18,322 cycles

AFT CARGO DOOR SILL WEB CORRODED. R & R WEB IAW AARD 51-10-05-1.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,191 hrs · 18,322 cycles

AUXILIARY POWER UNIT INLET AT STATION 1121 VERTICAL STIFFENER CORRODED. REPLACED STIFFENER YAW AARD 51-10-0-1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,191 hrs · 18,322 cycles

AUXILIARY POWER UNIT INLET UPPER ANGLE AT STATION 1088 CORRODED. REPLACED ANGLE IAW AARD 51-10-05-1.

Part: FILLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,191 hrs · 18,322 cycles

FILLER AT STATION 1088 CORRODED. REPLACED FILLER.

Part: OVEN — OVERHEATED (GALLEY) · airframe 40,452 hrs · 16,437 cycles

PHX - INFLIGHT MCO-LAX. CREW REPORTED FIRST CLASS OVEN OVERHEATED. FLIGHT ATTENDANT PULLED CIRCUIT BREAKER AND WALL STAYED HOT. EMERGENCY DECLARED FLIGHT DIVERTED PHX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED FORWARD GALLEY OVEN AND CHECKED WALLS, CANNON PLUG AND CIRCUIT BREAKER FOR HEAT DAMAGE WITH NONE FOUND. REINSTALLED OVEN AND PLACARD FOWARD GALLEY OVEN PER NEF. REPLACED OVEN AT ORD ON 10/14/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 40,421 hrs · 16,426 cycles

LEFT ELEVATOR HAS 10 EACH CRACKS ON UPPER SURFACE. ACCOMPLISHED 200 DEGREE WET LAYUP INTERIM REPAIR PER SRM 55-20-01-2R 1 ELEVATOR AND EA B737-55-026430.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 40,421 hrs · 16,426 cycles

RIGHT ELEVATOR HAS 13 CRACKS ON UPPER SURFACE. ACCOMPLISHED 200 DEGREE WET LAYUP INTERIM REPAIR PER SRM 55-20-01-2R 1 AND EA B737-55-026430.

Part: SKIN — SCRATCHED (HORIZ STAB) · airframe 40,421 hrs · 16,426 cycles

SCRATCH TO LEFT STABILIZER LOWER SURFACE STATION 168, 10 INCHES AFT OF LEADING EDGE. INSTALLED DOUBLER REPAIR PER SRM 55-10-01-2R.

Part: SKIN PANEL — DAMAGED (TE FLAP) · airframe 40,421 hrs · 16,426 cycles

AN INTERIM REPAIR WAS ACCOMPLISHED ON THE UPPER LEFT CORNER FASTENER HOLE OF THE LEFT INBOARD MAIN FLAP UPPER SKIN PANEL. INSTALLED PERMANENT EXTERNAL DOUBLER REPAIR AS PER EA B737-57-026476.

Part: SENSOR — FAULTED (LE SLAT) · airframe 39,298 hrs · 15,963 cycles

MIA - CREW REPORTED LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED. RAN CHECKLIST WITH NO RESULTS. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND SLAT NUMBER 3 INBOARD SENSOR FAULTING. REPLACED SENSOR S999. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ENGINE — FAILED (LEFT) · airframe 37,096 hrs · 15,056 cycles

SFO - CREW REPORTED LOUD BANG FROM LEFT ENGINE. LEFT ENGINE SHUTDOWN SINGLE ENGINE TIME (19 MINS). EMERGENCY DECLARED FLIGHT RETURNED SFO LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT SFO ON 08/15/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN) · airframe 34,951 hrs · 14,233 cycles

EMERGENCY LIGHT AT 18DEF INOPERATIVE. SECURED LOOSE CONNECTOR AT 18DEF. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,988 hrs · 13,872 cycles

PASS CABIN LIGHTING EMERGENCY CHARGER RIGHT AFT FAILED SIC 2908. REPLACED BATTERY PACK.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 33,778 hrs · 13,792 cycles

TOOLING MARK AT FRAME 727 LEFT SIDE BETWEEN STRINGERS 20 AND 21. REPAIRED PER SRM 51-70-11-2R.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 33,778 hrs · 13,792 cycles

OIL CANNING ON AFT PRESSURE BULKHEAD LOCATED TOP UPPER SECTION APROXIMATELY 4 INCHES LEFT OF CENTERLINE. REPAIRED PER EA B737-53-011357.

Part: WEB — DAMAGED (FUSELAGE) · airframe 33,778 hrs · 13,792 cycles

COCKPIT FLOOR HAS HEAVY CREASE AFT OF PILOTS SEAT. ACCOMPLISHED WEB REPAIR PER SRM 51-70-13-2R.

Part: FLAP — CRACKED (WING) · airframe 33,778 hrs · 13,792 cycles

CRACK AT NUMBER 2 HINGE SUPPORT ON NUMBER 1 KRUEGER FLAP. EXTERNAL DOUBLER REPAIR AS PER SRM 57-43-02-2R 2.

Part: ACTUATOR — FAULTED (RT ENGINE) · airframe 33,362 hrs · 13,610 cycles

MIA - CREW REPORTED AIRCRAFT LOST THE RIGHT ENGINE BLEED AND LOSS OF CABIN PRESSURE. O2 MASKS DID DROP. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT HAND ENGINE VARIABLE STATOR VANE ACTUATOR. REPLACED O2 GENERATORS (MPN S417T40144). SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,142 hrs

MIA - EMERGENCY LIGHT AT WING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT WING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 26,845 hrs

DFW - EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. RESEATED CONNECTOR AT SIDEWALL FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROLLER — OVERHEATED (WINDOW HEAT) · airframe 25,703 hrs

STL INFLIGHT T1252/16NOV - OVERHEAD INDICATION FOR LEFT FRONT WINDOW ILLUMINATED FOLLOWED BY MULTIPLE CRACKS IN LEFT FRONT WINDOW. LANDED STL WITHOUT INCIDENT. REPLACED WINDOW AND WINDOW HEAT CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

TUL - EMERGENCY LIGHTS IN MID COACH CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT 19A FOR EMERGENCY LIGHTS AT MID COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT AFT OVERWING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

TUL - CABIN EMERGENCY LIGHT BATTERY PACK AT STATION 566 FAILED TEST PER CARD 2904. REPLACED BATTERY PACK AT STATION 566 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

TUL - CABIN EMERGENCY LIGHT BATTERY PACK AT STATION 500 FAILED TEST PER CARD 2904. REPLACED BATTERY PACK AT STATION 500 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

TUL - CABIN EMERGENCY LIGHT BATTERY PACK FAILED TEST PER CARD 2904. REPLACED BATTERY PACK AT STATION 727 FOR CABIN EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SIGN — BROKEN (CABIN)

MIA - EMERGENCY EXIT SIGN AT 4R DOOR BROKEN. REPLACED EMERGENCY EXIT SIGN AT 4R DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 20 INOPERATIVE. SPLICED WIRE AT RIGHT SIDEWALL ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROW 20-21 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT WIRE SPLICES AT ROW 19-20 AND RESET PINS IN EMERGENCY EXIT LIGHT CONNECTOR. (M)

Part: LIGHT — MISSING (CABIN)

MIA - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT LIGHT AT FIRST CLASS GALLEY MISSING. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — OUT OF ADJUST (LT EMERG EXIT)

DTW - FLT 1183 - ON TAKEOFF ROLL AT APPROXIMATELY 60 KNOTS, LEFT FORWARD OVERWING EMERGENCY EXIT DOOR LIGHT ILLUMINATED IN COCKPIT. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. RESET SWITCHES ON LEFT FORWARD OVERWING EMERGENCY EXIT DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)